The effect of an end plate boundary layer on half delta wing flows at low Reynolds number

Vortical flows over delta wings

Riley, A.J.

January 1996

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN010193 / BLDSC - British Library D...

The effects of rounding the leading edges on the characteristics of separated flow past delta wings of low aspect ratio

Zakharovi, S
Royal Aerospace Establishment, Farnborough (United Kingdom)

January 1990

Report also known as RAE-Trans--2164Available from British Library Document Supply Centre- DSC:0678....

Boundary layer transition in simulated turbine blade flow

Graham, D
Dundee Institute of Technology (United Kingdom)
Council for National Academic Awards (CNAA), London (United Kingdom)

January 1990

SIGLEAvailable from British Library Document Supply Centre- DSC:DX94436 / BLDSC - British Library Do...

The effect of an end plate boundary layer on half delta wing flows at low Reynolds number.

Alkhozam, Abdullah M

August 2000

An experimental investigation has been carried out to study and understand the influence of an end p...

Boundary-layer effects in liquid-layer flows

Brotherton-Ratcliffe, R.V

January 1987

SIGLEAvailable from British Library Document Supply Centre-DSC:DX191950 / BLDSC - British Library Do...

Boundary-layer transition and heat transfer on slender delta wings

Poll, D
Manchester Univ. (United Kingdom). Dept. of Engineering

January 1989

Report also MU-DE-AR--8904Available from British Library Document Supply Centre- DSC:6015.42F(N--92-...

Some effects of transpiration on the boundary layer at the leading edge of a swept wing

Smith, A.

January 2000

Available from British Library Document Supply Centre-DSC:DXN049905 / BLDSC - British Library Docume...

Low Reynolds number turbulent boundary layers and wakes

Gough, T.

January 1996

Available from British Library Document Supply Centre-DSC:DXN012365 / BLDSC - British Library Docume...

Low speed aerodynamic characteristics of 60 degree rounded leading-edge delta wing with vortex flaps part 1 457mm span delta wing

Rinoie, K.
College of Aeronautics, Cranfield (United Kingdom)

January 1996

SIGLEAvailable from British Library Document Supply Centre-DSC:3310.760(9611) / BLDSC - British Libr...

The stability of the boundary layer on swept wings

Taylor, M.J.

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:D199865 / BLDSC - British Library Doc...

The effect of Reynolds number and wall roughness on bursts in turbulent boundary layers

Westbury, P.S.

January 1996

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN010893 / BLDSC - British Library D...

On the unsteady boundary layer and wake of a flat plate, and modelling water flow near a ship-side

Papadopoulos, D.

January 2000

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN037854 / BLDSC - British Library D...

Turbulent boundary layer flow over undulating surfaces

Belcher, S.E

January 1990

SIGLEAvailable from British Library Document Supply Centre- DSC:D60148 / BLDSC - British Library Doc...

Turbulent boundary layers on mildly curved surfaces

Muck, K.C.

January 1982

SIGLEAvailable from British Library Document Supply Centre-DSC:DX201895 / BLDSC - British Library Do...

Low speed aerodynamic characteristics of 60 degree rounded leading-edge delta wing with vortex flaps part 2 1.15m span delta wing (effect of flap deflection angle and leading-edge radius)

Rinoie, K.
College of Aeronautics, Cranfield (United Kingdom)

January 1996

SIGLEAvailable from British Library Document Supply Centre-DSC:3310.760(9612) / BLDSC - British Libr...

Vortical flows over delta wings

Riley, A.J.

January 1996

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN010193 / BLDSC - British Library D...

The effects of rounding the leading edges on the characteristics of separated flow past delta wings of low aspect ratio

Zakharovi, S
Royal Aerospace Establishment, Farnborough (United Kingdom)

January 1990

Report also known as RAE-Trans--2164Available from British Library Document Supply Centre- DSC:0678....

Boundary layer transition in simulated turbine blade flow

Graham, D
Dundee Institute of Technology (United Kingdom)
Council for National Academic Awards (CNAA), London (United Kingdom)

January 1990

SIGLEAvailable from British Library Document Supply Centre- DSC:DX94436 / BLDSC - British Library Do...

The effect of an end plate boundary layer on half delta wing flows at low Reynolds number.

Alkhozam, Abdullah M

August 2000

An experimental investigation has been carried out to study and understand the influence of an end p...

Boundary-layer effects in liquid-layer flows

Brotherton-Ratcliffe, R.V

January 1987

SIGLEAvailable from British Library Document Supply Centre-DSC:DX191950 / BLDSC - British Library Do...

Boundary-layer transition and heat transfer on slender delta wings

Poll, D
Manchester Univ. (United Kingdom). Dept. of Engineering

January 1989

Report also MU-DE-AR--8904Available from British Library Document Supply Centre- DSC:6015.42F(N--92-...

Some effects of transpiration on the boundary layer at the leading edge of a swept wing

Smith, A.

January 2000

Available from British Library Document Supply Centre-DSC:DXN049905 / BLDSC - British Library Docume...

Low Reynolds number turbulent boundary layers and wakes

Gough, T.

January 1996

Available from British Library Document Supply Centre-DSC:DXN012365 / BLDSC - British Library Docume...

Low speed aerodynamic characteristics of 60 degree rounded leading-edge delta wing with vortex flaps part 1 457mm span delta wing

Rinoie, K.
College of Aeronautics, Cranfield (United Kingdom)

January 1996

SIGLEAvailable from British Library Document Supply Centre-DSC:3310.760(9611) / BLDSC - British Libr...

The stability of the boundary layer on swept wings

Taylor, M.J.

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:D199865 / BLDSC - British Library Doc...

The effect of Reynolds number and wall roughness on bursts in turbulent boundary layers

Westbury, P.S.

January 1996

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN010893 / BLDSC - British Library D...

On the unsteady boundary layer and wake of a flat plate, and modelling water flow near a ship-side

Papadopoulos, D.

January 2000

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN037854 / BLDSC - British Library D...

Turbulent boundary layer flow over undulating surfaces

Belcher, S.E

January 1990

SIGLEAvailable from British Library Document Supply Centre- DSC:D60148 / BLDSC - British Library Doc...

Turbulent boundary layers on mildly curved surfaces

Muck, K.C.

January 1982

SIGLEAvailable from British Library Document Supply Centre-DSC:DX201895 / BLDSC - British Library Do...

Low speed aerodynamic characteristics of 60 degree rounded leading-edge delta wing with vortex flaps part 2 1.15m span delta wing (effect of flap deflection angle and leading-edge radius)

Rinoie, K.
College of Aeronautics, Cranfield (United Kingdom)

January 1996

SIGLEAvailable from British Library Document Supply Centre-DSC:3310.760(9612) / BLDSC - British Libr...

Vortical flows over delta wings

Riley, A.J.

January 1996

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN010193 / BLDSC - British Library D...

The effects of rounding the leading edges on the characteristics of separated flow past delta wings of low aspect ratio

Zakharovi, S
Royal Aerospace Establishment, Farnborough (United Kingdom)

January 1990

Report also known as RAE-Trans--2164Available from British Library Document Supply Centre- DSC:0678....

Boundary layer transition in simulated turbine blade flow

Graham, D
Dundee Institute of Technology (United Kingdom)
Council for National Academic Awards (CNAA), London (United Kingdom)

January 1990

SIGLEAvailable from British Library Document Supply Centre- DSC:DX94436 / BLDSC - British Library Do...

The effect of an end plate boundary layer on half delta wing flows at low Reynolds number

Abstract

Extracted data

The effect of an end plate boundary layer on half delta wing flows at low Reynolds number

Abstract

Extracted data

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